EP3141378A2 - System und verfahren zur steuerung wenigstens einer variablen während des layups eines verbundstoffteils mithilfe automatisierter faserplatzierung - Google Patents

System und verfahren zur steuerung wenigstens einer variablen während des layups eines verbundstoffteils mithilfe automatisierter faserplatzierung Download PDF

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Publication number
EP3141378A2
EP3141378A2 EP16183108.6A EP16183108A EP3141378A2 EP 3141378 A2 EP3141378 A2 EP 3141378A2 EP 16183108 A EP16183108 A EP 16183108A EP 3141378 A2 EP3141378 A2 EP 3141378A2
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EP
European Patent Office
Prior art keywords
automated
fiber tows
layup
laminate
weight
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP16183108.6A
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English (en)
French (fr)
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EP3141378B1 (de
EP3141378A3 (de
Inventor
Christopher James Madsen
Ram Kumar Upadhyay
Stefaan Guido Van Nieuwenhove
Thomas Kluge
Mathias Ernst Messmer
Martin Petersen
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General Electric Co
Original Assignee
General Electric Co
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Filing date
Publication date
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Publication of EP3141378A2 publication Critical patent/EP3141378A2/de
Publication of EP3141378A3 publication Critical patent/EP3141378A3/de
Application granted granted Critical
Publication of EP3141378B1 publication Critical patent/EP3141378B1/de
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/382—Automated fiber placement [AFP]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/382—Automated fiber placement [AFP]
    • B29C70/384—Fiber placement heads, e.g. component parts, details or accessories
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • B29C70/388—Tape placement heads, e.g. component parts, details or accessories
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
    • G01N21/84—Systems specially adapted for particular applications
    • G01N2021/8472—Investigation of composite materials
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
    • G01N21/84—Systems specially adapted for particular applications
    • G01N21/8422—Investigating thin films, e.g. matrix isolation method

Definitions

  • the disclosure relates generally to automated fiber placement systems and methods and, more particularly, to a system and method for controlling one or more variables during fabrication of composite parts using automated fiber placement.
  • the present disclosure includes an automated in-line manufacturing system and a method for controlling the thickness and weight of a composite part manufactured using the automated in-line manufacturing system.
  • an automated in-line manufacturing system for controlling at least one variable during layup of a composite part using automated fiber placement.
  • the automated in-line manufacturing system including an automated layup system and a controller.
  • the automated layup system is configured to receive a feed-through of one or more fiber tows as an input material and provide layup of the one or more fiber tows to form a laminate of one or more laid up plies.
  • the controller is configured to respond to measurement data obtained in one or more samplings and adjust the layup of the one or more fiber tows to compensate for a variation from one or more of a reference weight of the input material and a reference weight of the laminate.
  • the automated in-line manufacturing system including an automated layup system and a controller.
  • the automated layup system is configured to receive a feed-through of one or more fiber tows as an input material and provide layup of the one or more fiber tows to form a laminate of one or more laid up plies.
  • the controller is configured to adjust at least one of a fiber tow length, and a change in a number of plies being laid up using feedback based on measurement data obtained in one or more samplings to compensate for a variation from one or more of a reference weight of the input material and a reference weight of the laminate.
  • Yet another aspect of the disclosure resides in a method for controlling the thickness and weight of a composite part manufactured using an automated in-line manufacturing system.
  • the method including:(a) laying up one or more fiber tows using an automated layup system to form a laminate of one or more laid up plies, the laying up process including adhering the one or more fiber tows to a surface of a substrate to form the laminate, the automated layup system configured to receive a feed-through of the one or more fiber tows as an input material; (b) obtaining measurement data in one or more samplings during the laying up of the one or more fiber tows; (c) responding to the measurement data to adjust the layup program of the one or more fiber tows to compensate for a variation from one or more of a reference weight of the input material and a reference weight of the laminate; and (d) repeating steps (a)-(c) until layup of the one or more fiber tows is complete.
  • a composite automated in-line manufacturing system 100 including an automated in-line layup system 105 and a controller 116 is disclosed for the layup of one or more fiber tows 112 to form a composite part 140, as described generally with reference to FIG. 1 .
  • the automated in-line manufacturing system 100 can be used for controlling the thickness and weight of a composite part 140, non-limiting examples of which include low weight, high strength aircraft and automotive parts.
  • FIG. 1 is a diagrammatic illustration of one embodiment of the automated in-line manufacturing system 100 in accordance with aspects of the present disclosure for layup of the one or more fiber tows 112, such as on to a substrate 114, to form a laminate 110 of one or more laid up plies 111.
  • the term "substrate” may include a film, a mold, a tool, or the like used for fabrication of a composite part.
  • the substrate 114 may be manually or automatically placed in the automated in-line manufacturing system 100 in a desired location.
  • the substrate may be operably provided with indicia, pins, or other suitable means for use in determining and/or aligning the substrate 114 relative to the automated in-line manufacturing system 100.
  • the automated in-line manufacturing system 100 may utilize pre-pregs, whereby the one or more fiber tows 112 are pre-impregnated with a resin system.
  • the automated in-line manufacturing system 100 may utilize dry fiber tows and include a means for delivering a resin, as described below.
  • the automated in-line manufacturing system 100 further comprises the controller 116, such as a computing unit or computer, operable for controlling the automated in-line manufacturing system 100, and more particularly a layup program 117.
  • the composite automated in-line manufacturing system 100 includes a fiber dispensing means 118 for feeding the one or more fiber tows 112, where each of the one or more fiber tows 112 is moving at a respective fiber speed.
  • the one or more fiber tows 112 are pre-impregnated with a resin, and commonly referred to as pre-pregs.
  • the fiber dispensing means 118 may be configured to separately feed each of the one or more fiber tows 112, such that the tows 112 can be fed at different rates or at the same rate, depending upon design parameters and in response to the controller 116 and the layup program 117.
  • the fiber dispensing means 118 is in communication with one or more spools 122 onto which each of the tows in the one or more tows 112 is initially wound on a respective one of the spools 122.
  • the one or more fiber tows 112 comprise any suitable reinforcing material, for example, relatively continuous fibers, or tows, may be arranged to form a unidirectional array of fibers.
  • suitable fibers to be included in such reinforcing materials include without limitation, glass fibers, carbon and graphite fibers, aramid fibers, basalt fibers, polymeric fibers, including aramide and boron filaments, silica fibers, copper fibers and the like.
  • the fibers may be non-conductive or conductive, depending upon the desired application of the composite fiber.
  • the one or more fiber tows 112 comprise carbon fibers.
  • the disclosure is not limited to these specific fiber types.
  • the composite automated in-line manufacturing system 100 further includes the controller 116.
  • the controller 116 is configured to respond to obtained measurement data (described presently) to provide adjustments to the automated in-line manufacturing system 100 based on a calculated required compensation.
  • measurement data may include one or more samplings of at least one of a weight of the input, or parent material, and more particularly the one or more fiber tows 112, and/or a weight of the laminate 110 during fabrication, and more particularly during buildup of the plies 111, that form the composite part 140.
  • the controller 116 is configured to adjust the layup and more particularly the feed-through of the one or more fiber tows 112, in response to the measurement data, to compensate for a variation from a reference weight of the input material or laminate during build. More particularly, based on the variance of the measurement data from the reference data, the controller 116, and more particularly a layup program 117 that is controlling the automated in-line manufacturing system 100 is adjusted and/or an additional layup program is added, to compensate for the variation during build.
  • Such adjustments may include, but are not limited to, one or more of a change in the number of plies being laid up to form the laminate 110 and/or a change in a length of the one or more fiber tows 112 within the automated in-line manufacturing system 100 using feedback based on measurement data of the one or more samplings.
  • the composite automated in-line manufacturing system 100 may include one or more sensors 130 for inline monitoring/sampling at least one of a weight of the input material, and more particularly the one or more fiber tows 112, and/or a weight of the laminate 110 during build.
  • a single sensor 130 is indicated in FIG. 1 , a plurality of sensor 130 may be employed, and in one non-limiting example, one sensor 130 is provided for each of the fiber tows 112.
  • Example sensors include optical or contact sensors.
  • the controller 116 may exchange information with the automated in-line manufacturing system 100 as indicated in FIG. 1 , to optimize the fabrication of the laminate 110 and thus the final composite part 140.
  • the controller 116 may be configured to adjust the number of plies 111 being laid up in the laminate 110 and/or a change a length of the one or more fiber tows 112 within the automated in-line manufacturing system 100.
  • the controller 116 may comprise one or more processors. It should be noted that the present disclosure is not limited to any particular processor for performing the processing tasks of the disclosure.
  • the term "processor,” as that term is used herein, is intended to denote any machine capable of performing the calculations, or computations, necessary to perform the tasks of the disclosure, and to control the mechanical and electrical devices in the disclosure.
  • the term "processor" is intended to denote any machine that is capable of accepting a structured input and/or of processing the input in accordance with prescribed rules to produce an output, as will be understood by those skilled in the art.
  • the automated in-line manufacturing system 100 further includes one or more clamping, feeding and guide components 124 and one or more cutting components 126 disposed in feed-through positioning with at least one compaction roller 132, configured to deliver a force to adhere the one or more fiber tows 112 to the layup surface 115 of the substrate 114 to form the laminate 110 of the one or more laid up plies 111.
  • the automated in-line manufacturing system 100 may further include a heater 134, a tow guide scoop 136 and a positioning system (not shown) to orient the compaction roller 132 relative to the layup surface 115 of the substrate 114.
  • the in-line manufacturing system 100 may be mounted on a robotic head (not shown) in front of the substrate 114, or mold, such that the one or more fiber tows 112 will adhere to the substrate 114 and pull the fiber feed through the system 100 when the automated in-line manufacturing system 100 moves with respect to the substrate 114.
  • the specific configuration of the composite automated in-line manufacturing system 100 may vary based on the application.
  • FIG. 2 illustrated is an alternate embodiment of a composite automated in-line manufacturing system, generally referenced 150, including an automated in-line layup system 105 and a controller 116.
  • a composite automated in-line manufacturing system 150 may utilize dry fiber tows, and thus further includes an automated resin delivery, deposition and infusion system 152.
  • the composite automated in-line manufacturing system 150 includes a fiber dispensing means 122 for feeding one or more fiber tows 112, where each of the fiber tows 112 is moving at a respective fiber speed.
  • the one or more fiber tows 112 are dry fiber tows.
  • the fiber dispensing means 118 may be configured to separately feed each of the one or more fiber tows 112, such that the tows 112 can be fed at different rates or at the same rate, depending upon design parameters and in response to the controller 116 and the calculated required layup compensation.
  • the one or more dry fiber tows 112 move from the clamping, feeding and guide components 124 to a resin delivery, deposition and infusion portion 154 of the automated resin delivery, deposition and infusion system 152.
  • the automated resin delivery, deposition and infusion system 152 includes the resin delivery, deposition and infusion portion 154 comprising a means for delivery, depositing and infusing a resin 156 onto the one or more fiber tows 112.
  • the resin delivery, depositing and infusion portion 154 is formed including separate components, but it should be understood that a single component delivery, deposition and infusion portion 154 is anticipated by this disclosure.
  • the disclosure is not limited to specific resins or fiber types. Additional aspects of an automated resin delivery, deposition and infusion systems and types of resins that may be utilized is further described in U.S. Patent application, entitled, “Resin Delivery, Application and Infusion System and Integrated Layup System and Method of Use", bearing attorney docket number 245652-1 and U.S. Patent Application serial no. 12/889,785 , filed by the same assignee, and incorporated herein by this reference.
  • any suitable reinforcing material may be infused using the apparatus, systems and methods described herein.
  • Useful fibers to be included in such reinforcing materials include without limitation, glass fibers, carbon and graphite fibers, aramid fibers, basalt fibers, polymeric fibers, including aramide and boron filaments, silica fibers, copper fibers and the like.
  • the fibers may be non-conductive or conductive, depending upon the desired application of the composite fiber.
  • the resin 156 is an epoxy resin
  • the one or more fiber tows 112 comprise carbon fibers.
  • the disclosure is not limited to these specific resins or fiber types.
  • the composite automated in-line manufacturing system 150 further includes a controller 116.
  • the controller 116 is configured to respond to measurement data to provide adjustments to the automated in-line manufacturing system 150, and more particularly the layup based on calculated required compensation.
  • measurement data may include one or more samplings of at least one of a weight of the input, or parent material, and more particularly the one or more fiber tows 112, and/or a weight of the laminate 110 during fabrication, or part build.
  • the controller 116 is configured to add an additional layup program and/or adjust the already present layup program 117, and thus the feed-through of the one or more fiber tows 112, in response to the measurement data, to compensate for a variation from a referenced weight of the input material, and more particularly the one or more fiber tows 112, or the laminate 110, from a predetermined reference weight. More particularly, based on the variance of the samples from the applicable reference, the controller 116, and more particularly the layup program 117 that is controlling the automated in-line manufacturing system 150, is adjusted to compensate for the variation of the one or more tows 112 or the laminate 110 during build.
  • Such adjustments may include, but are not limited to, a change in the number of plies being laid up to form the laminate 110, a change in a length of the one or more fiber tows 112, within the automated in-line manufacturing system 150, and/or control of a flow rate or an amount of the resin 156 through the automated resin delivery, deposition and infusion system 152, using feedback based on measurement data of the one or more samplings.
  • the composite automated in-line manufacturing system 150 may include one or more sensors 130 for inline monitoring/sampling at least one of a weight of the input material, and more particularly the one or more fiber tows 112, and/or a weight of the laminate 110 during build within the automated in-line manufacturing system 150 during fabrication.
  • the controller 116 may adjust the layup program 117 and/or add an additional layup program, to optimize the fabrication of the laminate 110 and thus the composite part 140. As stated, the controller 116 may be configured to adjust the number of plies being laid up in the laminate 110, change a length of the one or more fiber tows 112, and/or control of a flow rate or an amount of the resin 156 through the automated resin delivery, deposition and infusion system 152.
  • the automated in-line manufacturing system 150 is disposed in feed-through positioning with the at least one compaction roller 132 configured to deliver a force to adhere the one or more fiber tows 112 to the layup surface 115 of the substrate 114 to form the laminate 110.
  • a positioning system 138 may be included to orient the compaction roller 132 relative to the layup surface 115 of the substrate 114.
  • the specific configuration of the composite automated in-line manufacturing system 150 may vary based on the application.
  • FIG. 3 illustrated is a method 200 of controlling the thickness and/or weight of a composite part manufactured using an automated in-line manufacturing system, such as the composite part 140 and the automated in-line manufacturing system 100 of FIG. 1 or 150 of FIG. 2 .
  • a number "x" of plies are laid up to form a laminate, wherein each ply comprises one or more fiber tows, such as the one or more fiber tows 112 of FIGs. 1 and 2 .
  • the process of laying up the plies includes adhering the one or more fiber tows 112 to a surface of a substrate, such as surface 115 of substrate 114 of FIGs.
  • the automated layup system is configured to receive a feed-through of the one or more fiber tows as an input, or parent, material.
  • a determination is made as to whether the layup of the plies is complete, as indicated at 218, or not complete, as indicated at 206. If not complete, the process of obtaining measurement data is commenced in a step 208 by taking one or more samples from the fiber tows at a known time "t x " and weighing the samples, in a step 210, to obtain the required measurement data.
  • a sampling from the fiber tows may be obtained, as the required measurement data, prior to the step of laying up the plies.
  • a response to the measurement data is accomplished next by initially calculating a required compensation of the layup process, in a step 212.
  • the step of calculating the required compensation includes taking the measurement data, and more specifically the weight of the input material at time "t x " during the layup process and determining a variation from a reference weight of the input material.
  • the step of calculating the required compensation includes taking the measurement data, and more specifically the weight of the input material at time "t x " during the layup process, and data regarding how much material is laid up at time "t x ", to calculate the total weight of the laminate as laid up at time "t x ".
  • the calculated weight of the laminate at time "t x " as laid up is compared to a reference weight of the laminate that is required at that stage (time "t x ") of the layup according to the component requirements.
  • the layup program is adjusted, or an additional layup program is added, in a step 214, in response to the calculated required compensation.
  • the method includes responding to the measurement data to compensate for a variation in the weight of the input material or the weight of the laminate that needs to be obtained at that stage (time "t x ") of the layup according to the component requirement.
  • the response maybe in the form of adjusting one or more of the layup length of the tows, changing the number of plies, or adjusting the amount of resin delivery when included as a part of the system.
  • Steps 202-214 are repeated, as indicated at 216, in a continuous process until a time in which the layup is determined to be complete, as in step 218.
  • the completed layup, and more particularly the laminate is prepared for curing, at step 220 that may include placing the laminate in a vacuum bag.
  • the laminate is next cured, in a step 222, and the final component is weighed, in a step 224.
  • FIG. 4 illustrated is an alternate method 250 of controlling the thickness and/or weight of a composite part manufactured using an automated in-line manufacturing system, such as the composite part 140 and the automated in-line manufacturing system 100 of FIG. 1 or 150 of FIG. 2 .
  • the substrate is weighed to obtain an initial weight.
  • the term "substrate” may be used to indicate a film, or the like, or the mold and/or tool used for fabrication of the composite part, as previously described.
  • a number "x" of plies are laid up, wherein each ply comprises one or more fiber tows, such as the one or more fiber tows 112 of FIGs.
  • the process of laying up the plies to form the laminate 110 includes adhering the one or more fiber tows 112 to a surface of the substrate, such as surface 115 of substrate 114 of FIGs. 1 and 2 , to form the laminate 100 and the final composite part, such as the composite part 140 of FIGs. 1 and 2 .
  • the automated layup system is configured to receive a feed-through of the one or more fiber tows as an input material.
  • a determination is made as to whether the layup of the one or more fiber tows, and more particularly the plies forming the laminate, is complete 268 or not complete 258.
  • the process of obtaining measurement data is commenced in a step 260 by initially weighing the substrate and weighing the not yet complete layup of plies, or laminate on the substrate.
  • a response to the measurement data is accomplished next by initially calculating a required compensation of the layup process, in a step 262.
  • the step of calculating the required compensation includes taking the measurement data, and more specifically the combined weight of the not yet complete layup of plies (laminate) and the substrate, and subtracting the weight of the substrate from the measured total weight to obtain the laminate weight at a time "t x ".
  • the calculated weight of the laminate at time "t x " as laid up is compared to a reference weight of the laminate that is required at that stage (time "t x ") of the layup according to the component requirements.
  • the layup program is adjusted and/or an additional layup program is added, in a step 264, in response to the calculated required compensation. More specifically, the method includes responding to the measurement data to compensate for a variation from the reference weight of the laminate that needs to be obtained at that stage (time "t x ") of the layup, according to the component requirement. These responses maybe in the form of one or more of adjusting the layup length of the tows, changing the number of plies, or adjusting the amount of resin delivery when included as a part of the system. Steps 254-264 are repeated, as indicated at 266, in a continuous process until a time in which the layup is determined to be complete, as in step 268. At this time, the completed layup is prepared for curing, at step 270 that may include placing the laminate in a vacuum bag. The laminate is next cured, in a step 272, and the final component is weighed, in a step 274.
  • FIG. 5 illustrated is yet another alternate embodiment of a method 300 of controlling the thickness and/or weight of a composite part manufactured using an automated in-line manufacturing system, such as the composite part 140 and the automated in-line manufacturing system 100 of FIG. 1 or 150 of FIG. 2 .
  • an automated in-line manufacturing system such as the composite part 140 and the automated in-line manufacturing system 100 of FIG. 1 or 150 of FIG. 2 .
  • a number "x" of plies are laid up, wherein each ply comprises one or more fiber tows, such as the one or more fiber tows 112 of FIGs. 1 and 2 .
  • the process of laying up the plies includes adhering the one or more fiber tows 112 to a surface of a substrate, such as surface 115 of substrate 114 of FIGs.
  • the automated layup system is configured to receive a feed-through of the one or more fiber tows as an input, or parent, material.
  • a determination is made as to whether the layup of the plies is complete, as indicated at 318, or not complete, as indicated at 306.
  • continuous inline measurement data is obtained of the input material, prior to layup, as indicated at step 308.
  • the continuously obtained measurement data provides for calculations to be performed, in a step 312, to provide for continuous compensation of the layup process 300.
  • the step of calculating the required compensation includes taking the continuously obtained measurement data, and more specifically the weight of the input material prior to the layup process, and identifying variations from a reference weight of the input material.
  • the layup program is continually adjusted during the layup process, in a step 314, in response to the calculated required compensation.
  • the method includes responding to the measurement data to compensate for a variation in the weight of the input material from the reference weight of the input material as required by the component requirements. These responses maybe in the form of one or more of adjusting the layup length of the tows, changing the number of plies, or adjusting the amount of resin delivery when included as a part of the system.
  • Steps 302-314 are repeated, as indicated at 316, in a continuous process until a time in which the layup is determined to be complete, as in step 318.
  • the completed layup is prepared for curing, at step 320 that may include placing the layup plies in a vacuum bag.
  • the completed layup is next cured, in a step 322, and the final component is weighed, in a step 324.
  • the disclosed composite automated in-line manufacturing system integrates the ability to build a part with reduced variation in thickness and weight distribution as compared with the input material.
  • the automated process of the present disclosure thus providing fabrication of complex composite structures with improved control and at lower cost than conventional fiber placement systems.
  • the process advantageously provides automation and the determination of required adjustments that can be embedded in the automated fiber placement program.
  • the composite automated in-line manufacturing system includes sufficient flexibility to accommodate multiple algorithms for adjustments responding to sample measurements.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
EP16183108.6A 2015-08-12 2016-08-05 System und verfahren zur steuerung wenigstens einer variablen während der schichtung eines verbundstoffteils mithilfe automatisierter faserablage Active EP3141378B1 (de)

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US14/824,348 US10399276B2 (en) 2015-08-12 2015-08-12 System and method for controlling at least one variable during layup of a composite part using automated fiber placement

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EP3141378A2 true EP3141378A2 (de) 2017-03-15
EP3141378A3 EP3141378A3 (de) 2017-05-03
EP3141378B1 EP3141378B1 (de) 2019-04-03

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US (1) US10399276B2 (de)
EP (1) EP3141378B1 (de)
JP (1) JP6505058B2 (de)
CN (1) CN106426979A (de)
BR (1) BR102016018528A2 (de)
CA (1) CA2938230C (de)

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EP3572216A1 (de) * 2018-05-24 2019-11-27 Bombardier Inc. Messvorrichtung und verfahren zur messung der spannung von kohlenstofffaserkabeln
WO2020094829A1 (de) * 2018-11-08 2020-05-14 Technische Universität Berlin Druckkopf für die additive fertigung von faserverbundwerkstoffen
DE102022116075A1 (de) 2022-06-28 2023-12-28 Conbility GmbH Kompaktiereinheit zum Kompaktieren von übereinander angeordneten und zumindest abschnittsweise erwärmten Faserverbundschichten, Ablegeeinheit, Herstellungssystem und Verfahren

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JP2020069731A (ja) * 2018-10-31 2020-05-07 三菱重工業株式会社 プリプレグ自動積層装置
WO2020161516A1 (en) 2019-02-08 2020-08-13 Toray Industries, Inc. Method for producing towpreg
JP7437173B2 (ja) 2020-02-05 2024-02-22 津田駒工業株式会社 自動繊維束配置装置
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WO2020094829A1 (de) * 2018-11-08 2020-05-14 Technische Universität Berlin Druckkopf für die additive fertigung von faserverbundwerkstoffen
DE102022116075A1 (de) 2022-06-28 2023-12-28 Conbility GmbH Kompaktiereinheit zum Kompaktieren von übereinander angeordneten und zumindest abschnittsweise erwärmten Faserverbundschichten, Ablegeeinheit, Herstellungssystem und Verfahren
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Publication number Publication date
JP6505058B2 (ja) 2019-04-24
EP3141378B1 (de) 2019-04-03
JP2017061140A (ja) 2017-03-30
US20170043539A1 (en) 2017-02-16
US10399276B2 (en) 2019-09-03
EP3141378A3 (de) 2017-05-03
CA2938230A1 (en) 2017-02-12
BR102016018528A2 (pt) 2017-08-08
CA2938230C (en) 2018-12-04
CN106426979A (zh) 2017-02-22

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